Computational analysis of vented supersonic exhaust nozzles using a multiblock/multizone strategy

Journal of Propulsion and Power

Volumn 9, Issue 6, 1993, Pages 834-839

  Carlson, John R ^a   Pao, S Paul ^a   Abdol Hamid, Khaled S ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b ANALYTICAL SERVICES AND MATERIALS INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPONENTS; COMPUTER APPLICATIONS; FLOW OF FLUIDS; NUMERICAL ANALYSIS;

COMPUTATIONAL ANALYSIS; MULTIZONE STRATEGY; SUPERSONIC; TRAILING EDGE SLOTS;

NOZZLES;

EID: 0027700965     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.23697     Document Type: Article

References (8)

1. Baker, V. D., Kwon, O., Vittal, B. V., and McKain, T. F., “Expendable Supersonic Exhaust Nozzle Concepts,” AIAA Paper 89-2927, July 1989.
2. Baker, V. D., Kwon, O., Vittal, B. V., Berrier, B., and Re, R., “Experimental Evaluation of Expendable Supersonic Nozzle Concepts,” AIAA Paper 90-1904, Jan. 1990.
3. Abdol-Hamid, K. S., “The Application of 3D Space Marching Scheme for the Prediction of Supersonic Free Jets,” AIAA Paper 89-2897, July 1989.
4. Abdol-Hamid, K. S., and Compton, W. B., “Supersonic Navier-Stokes Simulations of Turbulent Afterbody Flows,” AIAA Paper 892194, July 1989.
5. Pao, S. P., and Abdol-Hamid, K. S., “Application of a New Adaptive Grid for Aerodynamic Predictions of Shock Containing Single Jets,” AIAA Paper 90-2025, July 1990.
6. Compton, W. B., Abdol-Hamid, K. S., and Abeyounis, W. K., “Comparison of Algebraic Turbulence Models for Afterbody Flows with Jet Exhaust,” AIAA Journal, Vol. 30, No. 11, 1992, pp. 2716-2722.
7. Carlson, J. R., “A Nozzle Internal Performance Prediction Method,” NASA TP-3221, Oct. 1992.
8. Eiseman, P. R., and Erlebacher, G., “Grid Generation for the Solution of Partial Differential Equations,” Inst, for Computer Applications in Science and Engineering Rept. NASA Langley Research Center, Hampton, VA, 1987.